Flow topology in compressible turbulent boundary layer

被引:66
|
作者
Wang, Li [1 ]
Lu, Xi-Yun [1 ]
机构
[1] Univ Sci & Technol China, Dept Modern Mech, Hefei 230026, Anhui, Peoples R China
基金
中国国家自然科学基金;
关键词
compressible boundary layers; turbulent boundary layers; DIRECT NUMERICAL-SIMULATION; VELOCITY-GRADIENT TENSOR; COHERENT VORTICAL STRUCTURES; NON-GAUSSIAN STATISTICS; RATE-OF-STRAIN; SCALE MOTIONS; EFFICIENT IMPLEMENTATION; EULER EQUATION; DYNAMICS; ENSTROPHY;
D O I
10.1017/jfm.2012.212
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The flow topologies of compressible turbulent boundary layers at Mach 2 are investigated by means of direct numerical simulation (DNS) of the compressible Navier-Stokes equations, and statistical analysis of the invariants of the velocity gradient tensor. We identify a preference for an unstable focus/compressing topology in the inner layer and an unstable node/saddle/saddle (UN/S/S) topology in the outer layer. The dissipation and dissipation production originate mainly from this UN/S/S topology. The enstrophy depends mainly on an unstable focus/stretching (UFS) topology, and the enstrophy production relies on a UN/S/S topology in the inner layer and on a UFS topology in the outer layer. The compressibility effect on the statistical properties of the topologies is investigated in terms of the 'incompressible', compressed and expanding regions. It is found that the locally compressed region tends to be more stable and the locally expanding region tends to be more dissipative. The compressibility is mainly related to unstable focus/compressing and stable focus/stretching topologies. Moreover, the features of the average dissipation, enstrophy, dissipation production and enstrophy production of the various topologies are clarified in the locally compressed and expanding regions.
引用
收藏
页码:255 / 278
页数:24
相关论文
共 50 条
  • [21] MHD compressible turbulent boundary-layer flow with adverse pressure gradient
    M. Xenos
    S. Dimas
    N. Kafoussias
    Acta Mechanica, 2005, 177 : 171 - 190
  • [22] Radiation effect on the turbulent compressible boundary layer flow with adverse pressure gradient
    Xenos, Michalis
    Pop, Ioan
    APPLIED MATHEMATICS AND COMPUTATION, 2017, 299 : 153 - 164
  • [23] Contribution of flow topology to the kinetic energy flux in hypersonic turbulent boundary layer
    Xu, Dehao
    Wang, Jianchun
    Yu, Changping
    Li, Xinliang
    Chen, Shiyi
    PHYSICS OF FLUIDS, 2022, 34 (04)
  • [24] THE LAMINAR BOUNDARY LAYER IN COMPRESSIBLE FLOW
    COPE, WF
    HARTREE, DR
    PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1948, 241 (827) : 1 - &
  • [25] TURBULENT FRICTION IN A BOUNDARY-LAYER OF COMPRESSIBLE GAS
    DOBROCHEEV, OV
    MOTULEVICH, VP
    THERMAL ENGINEERING, 1987, 34 (10) : 549 - 552
  • [26] HEAT TRANSFER IN COMPRESSIBLE TURBULENT BOUNDARY LAYER.
    Bauer, K.
    Winkler, W.
    Grigull, U.
    1978,
  • [27] The numerical decomposition of turbulent fluctuations in a compressible boundary layer
    Borodai, SG
    Moser, RD
    THEORETICAL AND COMPUTATIONAL FLUID DYNAMICS, 2001, 15 (01) : 35 - 63
  • [28] GRAPHICAL SOLUTION FOR TURBULENT BOUNDARY LAYER IN COMPRESSIBLE FLUIDS
    MARTIN, JJ
    JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (02): : 147 - 148
  • [29] Temperature Recovery Factor in a Compressible Turbulent Boundary Layer
    A. I. Leontiev
    V. G. Lushchik
    M. S. Makarova
    S. S. Popovich
    High Temperature, 2022, 60 : 409 - 431
  • [30] Temperature Recovery Factor in a Compressible Turbulent Boundary Layer
    Leontiev, A. I.
    Lushchik, V. G.
    Makarova, M. S.
    Popovich, S. S.
    HIGH TEMPERATURE, 2022, 60 (03) : 409 - 431